Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 14 cotter pin 27-92-13 01 -050 14 cotter pin 27-92-13 01A-050 R 18 cotter pin 27-92-13 01 -050 18 cotter pin 27-92-13 01A-050 R 22 cotter pin 27-92-13 01 -050 22 cotter pin 27-92-13 01A-050
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-34-00-710-001 Operational Test of the Elevator and Hydraulic
Actuation 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply 55-13-11-000-001 Removal of the THS Trailing Edge Access Panels 55-13-11-400-001 Installation of the THS Trailing Edge Access Panels 27-92-13-991-001 Fig. 401
3. Job Set-up
__________
Subtask 27-92-13-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the elevators and the trimmable horizontal stabilizer controls are set to the neutral position.
(2)
Make sure that the hydraulic systems are pressurized (Ref. TASK 29-10-00-863-001), (Ref. TASK 29-10-00-863-002), (Ref. TASK 29-10-00-863-003).
(3)
Make sure that the PIN-SIDE STICK LOCKING is in the CAPT and F/O side stick controllers.
(4)
Make sure that the warning notices are in the flight compartment to tell persons not to operate the flight controls.
(5)
Make sure that the warning notices are in position to tell persons not to operate the hydraulic systems.
(6)
Make sure that the access platforms are in position at zone 334 and/or zone 344.
(7)
Make sure that the horizontal stabilizer trailing edge access panels 334BT,334DB and/or 344BT,344DB are open (Ref. TASK 55-13-11-000-001).
Subtask 27-92-13-865-054
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
1EFF : ALL 1 27-92-13Page 408 1 1 May 01/00R 1 1 1CES 1
4. Procedure
_________ Subtask 27-92-13-420-050
A. Installation of the Elevator Position Transducer
(Ref. Fig. 401/TASK 27-92-13-991-001)
WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,
_______ REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
(1)
Hold the mounting bracket (15) and put the elevator position transducer (1) in position.
(2)
Install the upper attachment bolt (19) thru the mounting bracket (15) and the elevator position transducer (1) and install the washer (20) and the nut (21).
(3)
Tighten the nut (21) and safety with cotter pin (22)
(4)
Install the lower attachment bolts (4) thru the elevator position transducer (1) and the mounting bracket (15) and install the washers
(16) and the nuts (17).
(5)
Tighten the nuts (17) and safety with cotter pin (18).
(6)
Install the mounting bracket (15) to its supports with the washers
(25) and the bolts (24).
(7)
Put the control rod (7) in position on the elevator position transducer (1).
(8)
Insert the rigging pin into the elevator position transducer (1). NOTE : The rigging pin is part of the elevator position transducer.
____
(9)
Install the bush (6).
(10)
Install the bolt (5). If the bolt cannot be installed easily, adjust the length of the control rod (7) as follows:
(a)
Release the locking nut and the locking washer.
(b)
Adjust the control rod eye-end. Make sure that the eye-end is in safety.
(c)
Engage the locking washer. Tighten the locking nut and safety with MISCELLANEOUS (Material No. 19-010).
(11)
Install the bolt (5), the washer (12) and the nut (13).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(17)
